Thermal Forming of Refractory Alloy Surgical Needles

ABSTRACT

A method of thermal forming of refractory alloy suture needles is disclosed. Needle blanks made from refractory alloys are used to form surgical needles, which are heated to a temperature above the ductile to brittle transition temperature but below the recrystallization temperature of the refractory alloy. The heated needle blanks are then mechanically formed into a surgical needle.

This patent application is related to commonly-assigned patentapplication Ser. No. ______ entitled “Thermal Forming of RefractoryAlloy Surgical Needles and Fixture and Apparatus” filed on even dateherewith and incorporated by reference.

FIELD OF ART

The field of art to which this invention pertains is surgical needles,in particular, methods of thermally forming refractory alloy sutureneedles.

BACKGROUND OF THE INVENTION

Surgical needles are well known in the surgical arts. Typically thesurgical needles are mounted to sutures, and used in a variety ofsurgical procedures for approximating tissue. It is important that thesurgical needles function under a variety of conditions encountered bysurgeons when performing procedures on patients. Surgical needles can beused for delicate surgical procedures with relatively soft and fragiletissues such as liver or lung surgery and for more robust proceduresinvolving harder and tougher tissues such as ophthalmic, plastic, orcoronary artery bypass graft surgery. Surgical needles are also used invarious orthopaedic surgical procedures. Surgical needles must be ableto penetrate tissue rapidly and efficiently with minimal surgeoninsertion force and minimal tissue trauma. It is particularly importantthat the surgical needle maintain its structural integrity throughmultiple cycles while tissue is being approximated by the surgeon.

Surgical needles may be made from a variety of materials that have therequired strength and manufacturability properties. Examples of thesematerials include various grades of stainless steel including, 420, 455,4310 and various grades of specialty martensitic-aged steels includingETHALLOY (Ethicon, Inc., Somerville, N.J.). Although needles made fromsuch conventional materials are capable of adequate performance, thereis a constant search for surgical needles having improved propertiesthat will benefit both the surgeon and the patient. Certain refractorymetals offer unique properties such as exceptional stiffness andstrength that impart desirable handling characteristics to sutureneedles. However, the room temperature formability of many refractoryalloys is limited and often substantially less than the formability ofother metals typically used in the manufacture of suture needles.Difficulties may thus arise in the manufacture of refractory alloysurgical needles as numerous steps in a conventional manufacturingprocess require substantial material ductility. Suture needle bodies areoften press-formed or coined to exhibit flattened sides to facilitategrasping and needle orientation within the suture needle drivers. Needlebodies formed to exhibit flattened sides may also impart modestimprovements in strength and stiffness to the suture needle. Needlepoints also may be coined to produce cutting edges desirable for thepenetration of certain tissues. Furthermore, needles are commonly curvedinto a variety of arcuate configurations, for example, ¼, ⅜, or ½ circledesigns, in order to facilitate certain surgical procedures. Thesurgical needles must be processed during manufacturing to provide forthe mounting of surgical sutures. One way of mounting sutures to asurgical needle is to drill a blind bore hole into the proximal end ofthe needle to receive the end of a surgical suture. For channel mountedsutures, as opposed to sutures mounted in a drilled bore hole in theproximal end of the needle, needle channels are typically coined orstamped into the proximal end of the suture needle. In either type ofmounting configuration, the proximal ends of the needles are typicallyswaged to maintain the suture end in the channel or the bore hole.

The forming of refractory alloys into suture needle materials has notbeen extensively investigated. Conventional needle forming methodstypically cannot be used with refractory alloys. For example, it isknown to use a method of forming a suture receiving hole in steelneedles by pressing a perforating tool into the base of suture needlewhile the needle material is heated to a temperature close to themelting temperature, Tm, between the hot forming and casting temperatureof the alloy. This method is deficient for use on refractory metals forseveral reasons. If an alloy is taken to a temperature near the meltingpoint of the alloy, recrystallization of the alloy is a distinctlikelihood. Indeed recrystallization commonly occurs at much lowertemperatures, for many alloys around 0.4 Tm. If refractory metals areheated to near their melting point, recrystallization of the workhardened microstructure occurs and the alloy can be expected to loseessential properties and even exhibit brittle characteristics at roomtemperature due to the effect of microstructural changes on the ductileto brittle transition temperature, DBTT. Secondly, such a process isapplicable to oxidation resistant alloys, however, this is not the casefor refractory alloys (especially those in the W—Re binary system) asthese alloys will readily oxidize at temperatures far below theirmelting points.

The previously described needle forming methods may impart substantialstresses to the needle material, and if the material exhibitsinsufficient ductility, cracking and or splitting of the suture needlemay occur. Many refractory alloys exhibit ductile to brittle transitiontemperatures (DBTT) above room temperature, and consequently the abilityto plastically deform these refractory alloys in the various surgicalneedle forming operations is substantially limited. However, once abovethe DBTT, plastic deformability of the refractory alloys increasessubstantially. Excessively high temperatures may however lead to therecrystallization and growth of the grain structure of the alloy,leading to a substantial change in properties that may be deleterious tothe performance of the suture needle.

Therefore, there is a need in this art for novel methods ofmanufacturing and forming refractory alloy suture needles.

BRIEF DISCLOSURE OF THE INVENTION

Accordingly, a novel method of thermal forming refractory alloy sutureneedles is disclosed. In the method, an alloy metal needle blank isprovided. The needle blank is made from a refractory metal alloy. Atleast a section of the needle blank is heated to a temperature above theductile to brittle transition temperature but below there-crystallization temperature of the alloy. The heated needle blank ismechanically formed into a surgical needle.

These and other aspects of the present invention will become moreapparent from following description and accompanying drawings.

BRIEF DESCRIPTION OF THE DRAWINGS

FIGS. 1A-C illustrate a schematic of a thermal forming process of thepresent invention utilizing resistive heating.

FIGS. 2A-C illustrate an alternate embodiment of the present inventionfor thermal forming needles from refractory alloys using a hot gasinjection system.

FIGS. 3A-C illustrate yet another alternate embodiment of the presentinvention for thermal forming of refractory alloy needles using aresistive heating element.

DETAILED DESCRIPTION OF THE INVENTION

Using the novel thermal forming processes of the present invention,refractory alloys used in the manufacture of suture needles are heatedto a temperature above their DBTT during the given forming operation toprovide substantial plastic deformation, but below the recrystallizationtemperature of the alloy to prevent compromise of the suture needleproperties. Several methods for the thermal treatment and forming ofsuture needle materials during needle forming operations are disclosed.Needles manufactured from refractory metal alloys treated using thenovel thermal forming treatment processes of the present inventionexhibit numerous potential improvements in needle performance includingenhanced resistance to bending, pronounced I-beam (i.e., structural) andneedle point designs that enhance strength, stiffness and penetrationperformance, improved ductility and toughness, and in situ colorationvia surface oxidation.

The following terms used in present specification are defined to havethe following meanings:

Ductile to Brittle Transition Temperature (DBTT)—Temperature above whicha substantial improvement in ductility of the alloy occurs. Within thisdisclosure the DBTT is determined as the temperature at which the alloyexhibits at least 5% elongation to break in a simple tensile test.

Refractory Alloy—alloy comprised of one or more or the elements: W, Mo,Re, Os, Ir, Ta, Nb, Zr, Y that exhibit a DBTT above room temperature.

Recrystallization Temperature—Temperature at which new grains will formin the microstructure of the alloy.

Ductility—ability of an alloy to withstand plastic deformation withoutbreaking.

Elongation to break—measurement of sample percent elongation in a simpletensile test, used to assess alloy ductility.

Simple Tension—tension applied in one dimension with other dimensionsbeing unconstrained.

Thermal forming—plastic forming conducted on a heated work piece.

Needle Blank—elongate piece of wire, a portion of which is converted viaa multitude of processes into the shape of a suture needle.

Yield Bending Moment—the amount of moment required to initiate plasticdeformation during bend tests (ASTM standard F-1840-98a)

Bending Stiffness (Stiffness in Bending)—resistance to elasticdeformation of a curved suture needle.

Elastic Deformation—deformation, strain, or displacement that isrecoverable by removing the applied load

I-beam Needle Body—any variety of needle body designs that incorporateflattened opposed sides (instead of an entirely rounded design)

Maximum Bending Moment—the greatest moment applied to needle during bendtest (ASTM standard F-1840-98a)

Materials Properties—Properties of the material only, derived by testingin a manner in which needle shape and surface properties do notinfluence data. Examples include: Young's modulus, ultimate tensilestrength (when tested in simple tension), and microhardness hardness.

Grain Structure—an assemblage of crystals that share a common atomicperiodicity and together as a multitude comprise the needle material.

Dislocation—a line defect within a grain structure that manifests itselfas a missing plane of atoms, that is commonly necessary to enableplastic deformation of metals at or near room temperature.

It should be noted the terms “surgical needle” and “suture needle” areused interchangeably herein.

The metal alloys useful in the practice of the present invention includeconventionally known refractory metal alloys including: tungsten,tungsten-rhenium, tungsten-osmium, molybdenum, molybdenum-rhenium,molybdenum-zirconium-titanium, iridium, and the like.

Rhenium additions can substantially improve the ductility of W—Realloys. Published results for arc melted W—Re alloys of varying Rheniumconcentration are disclosed in NASA technical publication (NASA TND-4567) entitled, “Yielding and Fracture in Tungsten andTungsten-Rhenium Alloys”. A tungsten 25% Rhenium alloy exhibitedsubstantial elongation to break near room temperature whereas a puretungsten sample exhibited no reportable elongation to break. Taking acloser look at the pure tungsten alloy, it was clear that a markedimprovement in elongation to break occurred over the temperature rangeof 520 to 600K. Over this temperature range the alloy transitioned frombrittle to ductile. A ductile to brittle transition temperature (DBTT)is often used to demarcate this transition in ductility, and while thisnomenclature is the norm in the field of metallurgy, the actuallytransition in materials performance does not typically occur at aprecise single temperature, but rather occurs over a range oftemperatures in a polycrystalline sample. The breadth of this DBTTtransition region may increase with Rhenium concentration, with highRhenium alloys showing a gradual slope up in elongation to break withtemperature as opposed to the more rapid change of the pure alloy.Nevertheless, it is clear that heat profoundly increases the ductilityexhibited by W—Re alloys. According to this NASA report, for a W-25% Realloy, the room temperature ductility approximately doubles at 500K andapproximately quadruples at 700K. For convenience, the author of thisNASA study chose the temperature at which the alloy exhibited 5%elongation to break as the ductile to brittle transition temperature(DBTT), or for the W-25% Re alloy, 350K. It should be noted that otherfactors such as alloy impurities, grain size, and work hardening historycan also impact the onset temperature of ductile behavior (and thereported value of the DBTT).

Suture needles are conventionally and most typically formed from wirethrough a multitude of conventional process steps including: wirestraightening, needle blank formation, point coining and/or pointgrinding, needle body forming, curving, suture receiving hole drilling,or channel forming, polishing, siliconization, and so on. The processsteps may include one or more conventional mechanical, chemical, heattreatment, and/or electrical sub-processes. Suture needle formingoperations often result in substantial plastic deformation of the needlematerial. Even alloys with high rhenium concentration exhibit limitedplastic deformation with elongation to break values rarely exceeding 7%at room temperature and more commonly less than 5%. This lack of roomtemperature ductility can limit the shape and design of the sutureneedle. In particular, suture needles are typically formed to exhibitrectangular cross-sectional shapes in the body or mid-section of theneedle. Such a rectangular cross-section facilitates grasping andcontrol of the suture needle with needle holders in addition toimparting a modest increase in strength and stiffness. In order to forma rectangular cross-section, a series of conventional coiningoperations, by which the needle is partially flattened between twoparallel opposing dies, is typically performed. These coining operationscan result in deformation strains that exceed the fracture limits of theW—Re alloy at room temperature. Likewise, needle points areconventionally coined using various conventional dies and conventionalcoining processes and equipment. A variety of conventional point designsmay be coined including but not limited to: taper point, cutting edge,or taper-cut varieties. Cutting edge needles generally provide the besttissue penetration performance with minimal tissue trauma. However,unlike taper point or taper cut needles that may be formed via asequence of grinding processes, cutting edge needles of optimal designrequire point coining operations that subject the needle material tosubstantial deformational strains, and consequently cracks in the needleblank can occur if forming is conducted below the DBTT of a refractoryalloy. In particular, cutting edge needles with radius hollow cuttingedges, as described by Smith et. al in U.S. Pat. No. 5,797,961A, whichis incorporated by reference, offer exceptional penetration performancewith minimal tissue trauma, but in production must be preformed via ahigh deformation coining operation. Other cutting edge needle pointdesigns for ophthalmic and micro surgery are similarly complex, andwhile offering exemplary tissue penetrating performance, also requirehigh deformation coining operations to produce. Finally, channels may beconventionally formed in the proximal end of suture needles tofacilitate suture attachment. This approach is particularly applicableto suture needles with wire diameters below ˜0.006″ that can beexceedingly difficult to mechanically drill or laser drill for thepurposes of producing a suture receiving hole. Substantial plasticdeformation commonly occurs during needle channel formation, and if arefractory alloy is formed at room temperature below its DBTT crackingwill likely occur.

The novel processes of the present invention enhance the formability ofrefractory metal alloys such as the tungsten alloys for the purposes ofproducing suture needles. These novel thermal forming processes of thepresent invention provide that a metal alloy suture needle blank beelevated to a temperature, just prior to or during a forming operation,that exceeds the DBTT (where the DBTT is determined as the temperatureat which the alloy exhibits at least 5% elongation to break in a tensiletest) but wherein the temperature is less than the recrystallizationtemperature of the alloy (where the recrystallization temperature isdefined for the purposes of this disclosure as any temperature thatleads to the formation of new grains in the microstructure of the alloy,during said forming operation). It is important to preventrecrystallization of the alloy, as a recrystallized microstructure willtypically exhibit lower tensile strength, and lower yield strength, bothof which are adverse to the handling and performance characteristics ofthe suture needle. Moreover, recrystallization of refractory alloys, inparticular tungsten alloys, often leads to the embrittlement of thealloy by further elevating the DBTT as a consequence of the eliminationof dislocations that occurs during recrystallization.

While mechanical forming of a refractory metal suture needle blank atelevated temperature may be necessary to prevent fracture, it is noteasily accomplished since equipment used in the manufacture of sutureneedles is expansive in nature employing several specialized formingstations that typically perform individual needle forming operationsserially one after the other, and this equipment cannot be, as a whole,subjected to elevated temperature for long without destroying itsfunction. This equipment is typically high speed precision equipment,and excessive heat could cause mechanical breakdowns of mechanicalcomponents. As such, heating of the refractory metal needle blank mustbe limited to a very small section of the equipment where heat resistantor water-cooled tooling can be used. Alternatively the heat used informing the needle blanks must be managed, for example to be turned onand then turned off with precise timing to heat predominantly the needleand not the surrounding tooling and equipment. Alternatively, thetooling may be actuated in such a way to substantially limit theduration of its exposure to the thermal forming zone.

Alternate embodiments of methods of the present invention for thermalforming needles in situ to heat an alloy metal needle blank during orimmediately prior to forming are illustrated in FIGS. 1-4, and describedherein. These methods include, but are not limited to: 1) resistiveneedle heating, 2) forced gas needle heating, 3) element controlledneedle heating, and 4) laser needle heating.

Referring first to FIGS. 1A-C, a resistive heating embodiment of theprocess of the present invention is illustrated. The forming die tool 10is seen to have lower tool base 20 and upper moveable member 40. Mountedrespectively to the inner surface 21 of tool base 20 and the innersurface 41 of moveable member 40 are the die members 50 each havinginner contact surfaces 51 for engaging the metal alloy needle blank 70.The tool 10 is seen to have a pair of opposed electrodes 80 havingcontact surfaces 81. The electrodes 80 are moveably mounted via springs90 to the tool base 20 and moveable member 40, respectively. Anelectrode 100 is mounted to the proximal end 71 of needle blank 70. Inthe resistive needle heating process, electrical contact is made acrossthe needle blank from the distal end 75 of needle blank 70 via theelectrodes 80 to the proximal end of the needle blank 71 via electrode100 and current is passed through the needle blank 70 to resistivelyheat it to the temperature desired for the forming operation. Electricalcontact can be made across the length of the needle blank 70 as theneedle blank 70 enters the die 10 or as it closes, as seen in FIGS.1A-C. Alternatively, current maybe passed through the thickness of theneedle blank 70 in the section in which forming will occur. Varioustraditional materials may be used to form the conducting electrodes 80(e.g. copper) used to make electrical contact and complete theelectrical circuit to allow current to pass through the needle blank 70.Optionally, the die members 50 may be used to make electrical contactand conduct the current, as many of the conventional tools such ascemented carbide tools typically used employ a continuous metal binderphase of substantial conductivity. The dies and/or electrical contactsmay be optionally liquid cooled to increase their performance andservice life. The amount of current passed through the needle blanks 70in the process of the present invention will be sufficient toeffectively heat the needle blank 70 to above its DBTT without inducingrecrystallization of the grain structure. The current will depend onwire diameter, composition of the refractory alloy, speed of the dieclosure, and other dynamic process factors, (and also upon electricalparameters such as voltage, frequency, etc.) but may typically be about1.0 amp to about 20.0 amps, more typically about 1.0 amp to about 10.0amps.

Another alternate embodiment of the process of the present inventionusing a forced gas thermal forming process is illustrated in FIGS. 2A-C.The forming die tool 110 is seen to have lower tool base 120 and uppermoveable member 140. Mounted respectively to the inner surface 121 oftool base 120 and the inner surface 141 of moveable member 140 are thedie members 150 each having inner contact surfaces 151 for engaging themetal alloy needle blank 170. With the forced gas method, a stream ofhot air or hot gas 160 is directed via guide 180 along the path of thealloy needle blank 170 as it enters and while it is positioned withinthe die assembly 110 between opposed die members 150. The guide 180 isseen to have needle guide section 182 and gas pathway section 185 thatintersect at junction 187. Since the needle blanks 170 are typicallysmall in diameter (between ˜1 and 60 mil) rapid convective heating ofthe needle blank 170 from the forced gas stream 160 may occur. As theneedle blank 170 reaches a predetermined forming temperature, the dies150 close and thermoform a segment 172 of the needle blank 170 to theprescribed shape, as seen in FIGS. 2 a-c. The gas used to heat thesuture needle may optionally be a shielding gas which would serve toprevent oxidation of the needle during the heating operation. Examplesof the gases that can be used include argon, helium, hydrogen, nitrogen,neon, carbon dioxide/carbon monoxide, or mixtures thereof. The velocityof the gas stream and the temperature of the gas stream will beeffective to sufficiently heat the refractory alloy above its DBTT whilepreventing recrystallization. The temperature of the needle during thethermoforming process will be sufficient to effectively enable plasticdeformation required in the forming operation without cracking orsplitting of the needle blank. The temperature will vary with the alloyselected to manufacture the needle blank. For a W—Re alloy needle blankthe temperature will typically range from 100 to about 1900° C., moretypically about 300 to about 1600° C., and preferably about 600 to about1400° C.

Still yet another embodiment of a thermal forming process of the presentinvention is illustrated in FIGS. 3A-C. The method utilizes a formedresistive heating element. The resistive element may be heated viadirect contact to an electrical circuit designed to pass current throughthe heating element. Alternatively, the resistive heating element may beheated by inductively coupling to a radio frequency magnetic field thatin turn induces an alternating current in the element to accomplishresistive heating. Either configuration generates radiant energy fromthe heating element to heat the suture needle. As seen in FIGS. 3A-C,the forming die tool 210 is seen to have lower tool base 220 and uppermoveable member 240. Mounted respectively to the inner surface 221 oftool base 220 and the inner surface 241 of moveable member 240 are thedie members 250 each having inner contact surfaces 251 for engaging themetal alloy needle blank 270. A resistive heating element 260 is seenpositioned within and about the die assembly in such a way that theheating element 260 fits around the working zone of the die 210, whilenot interfering with the motion of the needle blank 270 as it enters andleaves the thermal forming zone, and also without interfering with themovement of the die members 250. The heating elements 260 may beelectrically or electronically controlled to turn on and off at theappropriate times as the dies open and close to prevent excessiveheating of the dies. As seen in FIGS. 3A-C, after the needle blank 270is heated to a sufficiently effective temperature, the die members 240engage the needle blank 270 to thermally form a section of the blank271. Alternatively or in addition to time control of the heatingelements, the dies and affected machine components may be optionallyliquid cooled to prevent excessive thermal damage. Also, the dies mayoptionally retract away from the heating element to a position where thetemperature does not cause degradation of the die material. Aspreviously described, the heating elements may be of the type thatprovide radiant heat (as would be the case for standard resistivelyheated elements, infrared heating elements, and inductively coupledheating elements), or may be in the form of an induction coil whereinthe induction coil produces radio frequency that couples directly withand inductively heats the needle blank. If an induction heating elementis used, it may be advantageously designed to couple effectively withand heat the needle blank, but not couple with the surrounding dies. Thedesired temperatures will be those as previously described above for theother thermal heating and forming processes.

Although not illustrated, another thermal forming process of the presentinvention utilizes laser controlled needle heating. As the name implies,this embodiment uses a focused intense laser light beam to rapidly heatsections of the needle blank that require mechanical forming. One ormore lasers may impinge upon the needle blank simultaneously to increasethe length of the hot zone. The lasers may also be directed back andforth rapidly across the length of the needle that will be formed.Alternatively the needle may be rotated as the laser impinges toincrease the heat-affected area.

It will be recognized that as the hot needle blank contacts the lowertemperature dies, or as the source of the thermal energy is shut-off,the needle blank will have a tendency to begin to cool. As such, all ofthe thermal forming processes described above should be designed in sucha way that the actual forming operation that results in plasticdeformation of the needle material occurs rapidly in comparison to therate at which the needle blank cools.

As an additional benefit associated with the novel thermal formingmethods of the present invention, alloys that may exhibit high DBTT canbe formed into suture needles. For example, in the W—Re alloy system,alloys with high rhenium concentrations tend to have lower DBTT thanalloys with low rhenium concentration. However, from a commercialperspective, rhenium has a high raw material cost and can be anexceedingly expensive component of the alloy. If the thermal formingmethods of the present invention are used, low rhenium concentrationsmay be used in lieu of high rhenium concentrations to realize asubstantial cost savings. An additional benefit is that the market pricefor the finished suture needle may in theory be reduced, as raw materialcosts no longer need to be passed on to the customer, and use of thetungsten alloys as suture needle materials may be expanded to a greaternumber of needle designs.

Furthermore, greater tolerances for impurities in the alloy (that havethe effect of elevating the DBTT) may be permissible if the thermalforming methods of the present invention are used. Yet anotherassociated benefit is that supplier availability may broaden, therebypossibly resulting in decreased material cost.

Still yet an additional benefit of use of the novel methods of thepresent is seen when a needle blank is curved to form a curved orarcuate suture needle with the shape or configuration of, for example,¼, ⅜, ½ circle. During the conventional needle curving process performedat room temperature, residual stresses are typically imparted to theneedle body that detrimentally impact the yield bend moment of theneedle. It is believed that heat treatment after the curving operationeliminates some or all of such residual stresses and substantiallyenhances the yielding bend moment of the needle. Thermal formingoperations to curve the suture needle at elevated temperatures (e.g. inexcess of 900° C.) may result in a similar improvement in yield bendmoment.

Heat treating methods for the coloration of refractory alloy sutureneedles via the formation of a thin native surface oxide may be appliedin conjunction with the in situ thermal forming methods of the presentinvention. Refractory alloy suture needles may thus be colored duringneedle manufacturing operations, thus eliminating the need for asubsequent thermal coloring step. Where coloration is a desired outcome,the use of a conventional shielding gas should be avoided, or used incombination with a conventional oxidizing gas. However, if coloration isnot desired, a shielding gas may be used.

The following examples are illustrative of the principles and practiceof the present invention, although not limited thereto.

EXAMPLE 1

Needle blanks comprised of a tungsten-26% rhenium alloy with a nominalstarting wire diameter of 0.203 mm were pressed between two opposingcarbide dies to produce parallel opposed body flats. The tungsten-26%rhenium material from which the needle blank was made was acquired fromToshiba Corporation (Yokohama, Japan) and exhibited a breaking strengthof 3450 MPa in wire form. A conventional pneumatic uniaxial press wasused for the experiments with flat carbide dies. The length of theneedle blank, over which body flats were formed, was at least 1 cm. Inone set of experiments the needle blanks were pressed to variousthicknesses at room temperature and visually examined for cracks at 30×magnification with a stereoscope. It was found that cracks could beformed longitudinally along the length of the wire when the body flatwas coined to a thickness equal to or less than ˜0.175 mm. In a parallelset of experiments, the W-26% Re needle blanks were resistively heatedimmediately prior to and during the pressing operation using theexperimental configuration similar to that depicted in FIG. 1. Aconventional AC variac was used to sufficiently deliver and adjust thecurrent through the needle blank. In this way the needle could beeffectively heated to above 1000° C. as evidenced by the yellow to whiteglow that was produced. The entire heating and pressing operation took˜1.5 seconds. Visual examination at 30× magnification was used to detectcracks. It was found that needles that were heated to above ˜1000° C.(yellow to white glow discharge) could be produced with body flats of0.15 mm or less without any visually detectable cracks.

EXAMPLE 2

In order to assess the ductility of the suture needles of Example 1, areshape test was performed wherein each needle was held near itsproximal end with suitable, conventional needle holders and bent backand forth through 180 degrees multiple times until fracture of theneedle occurred. Each bend though 90 degrees from the initial shape ofthe needle was given a ½ count. The total number of counts is a measureof ductility with the higher numbers indicating greater ductility. Mostsuture needles are required by their manufacturers to exhibit a reshapevalue of at least 1.0. The W-26% Re suture needles made in Example 1above exhibited reshape values in excess of 4.0 thereby meeting andexceeding the standard requirement.

The novel methods of the present invention for thermoforming surgicalneedles have numerous advantages and benefits. These advantages andbenefits include: production of refractory alloy suture needles withflattened or I-beam body sections, coined needle points, and suturereceiving channels without cracking or splitting the needle blank andwithout compromising ductility and toughness of the suture needle,improved resistance to bending, stiffness, and strength via thermalcurving of the suture needle, coloration of the needle surface vianative surface oxide formation in situ during thermal forming negatingthe need for subsequent coloration processes, and selection of lowercost refractory alloys with high DBTT.

Although this invention has been shown and described with respect todetailed embodiments thereof, it will be understood by those skilled inthe art that various changes in form and detail thereof may be madewithout departing from the spirit and scope of the claimed invention.

1. A method of forming a refractory alloy into a surgical needle, saidmethod comprising: providing an alloy metal needle blank, said needleblank comprising a refractory metal alloy; heating at least a section ofthe needle blank to a temperature above the ductile to a brittletransition temperature, but below the recrystallization temperature ofthe alloy; and, mechanically forming the needle blank into a surgicalneedle.
 2. The method of claim 1 wherein the temperature is betweenabout 100° C. to about 1600° C.
 3. The method of claim 1 wherein thetemperature is between about 600° C. and about 1400° C.
 4. The method ofclaim 1 wherein the elongation to break of the alloy is increased toexceed 5%.
 5. The method of claim 1 wherein the forming operation isselected from the group consisting of needle body forming, needle pointcoining, needle channel coining, and needle curving.
 6. The method ofclaim 1 wherein the alloy has a Rhenium concentration comprising ofabout 0% to about 30%
 7. The method of claim 1 wherein the needle isheated using hot gas jets.
 8. The method of claim 1 wherein the needleis heated using a resistive heating element.
 9. The method of claim 1wherein the needle is heated by contacting electrodes to the needleblank and causing an electrical current to flow through the needleblank.
 10. The method of claim 1 wherein the needle is in an oxygen freeatmosphere when at an elevated temperature.
 11. The method of claim 10wherein the oxygen free atmosphere is a shielding gas or combination ofshielding gases selected from the group consisting of nitrogen, argon,helium, and hydrogen.
 12. The method of claim 1 wherein the refractoryalloy comprises Tungsten and one or more elements selected from thegroup consisting of Rhenium, Molybdenum, Tantalum, Titanium, Yttrium,Zirconium, and Niobium.
 13. The method of claim 1 wherein the refractoryalloy comprises Molybdenum and one or more elements selected from thegroup consisting of Rhenium, Tungsten, Tantalum, Osmium, Iridium,Yttrium, Zirconium, and Niobium.
 14. The method of claim 1 wherein therefractory alloy is Tungsten-Rhenium (W—Re).
 15. The method of claim 14wherein the W—Re alloy has a rhenium concentration less than 30% andpreferably 26% or less.
 16. The method of claim 14 wherein thetemperature of the W—Re alloy is elevated to between 100° C. and 1600°C. and more preferably between about 600° C. and 1400° C. where theforming operation is selected from the group consisting of coining,flattening, channel forming, point forming, and curving.
 17. The methodof claim 1 wherein the alloy needle blank is heated by a method selectedfrom the group consisting of resistive heating, radiant heat, inductioncoils, and hot gas streams.
 18. A surgical needle comprising arefractory alloy wherein the needle can be re-shaped more than 1.0 timeswithout breaking.
 19. The needle of claim 18 wherein the suture needlemade from a refractory alloy wire is work hardened to a tensile strengthgreater than 2500 MPa and thermal formed.